|  |  |  |
| --- | --- | --- |
|   | (d) | The installed components as a group will have an average of total flight time since new of not more than that of the Airframe;  |

  




|  |  |  |
| --- | --- | --- |
|   | (e) | Each Airframe Life-Limited Component will have not less than the Minimum Component Flight Hours and the Minimum Component Cycles remaining to next expected removal and will be
supported by certification documentation necessary to demonstrate Back-to-Birth Traceability; for this purpose “Airframe-Life Limited Component” means a component with an ultimate life which cannot be restored through appropriate
maintenance; for this purpose “Back-To-Birth Traceability” means certified documentation necessary to identify precisely where, when and with which aircraft operator the expired life and previous maintenance in relation to the Airframe
Life-Limited Component occurred since such Airframe Life Limited Component was new.  |

  




|  |  |
| --- | --- |
| **1.4** | **ENGINES**  |

  




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| --- | --- | --- |
|   | (a) | Each Engine (or a Replacement Engine as and to the extent permitted by Section 1.2(b) of this Schedule 6) will be installed on the Aircraft and comply with the following:
 |

  

 Each Engine will have not less than the Minimum
Engine Flight Hours and Minimum Engine Cycles expected life remaining to the next expected removal and the life limited Parts shall have not less than the Minimum Engine LLP Cycles release life remaining. The expected life remaining will be
determined by the inspection and checks accomplished by Lessor in accordance with the Lease which shall include the following: